Similarly shaped airfoils to DP1.68/8.37_DS
New! Bulk download of polars in Excel format: DP1.68_8.37_DS.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (0) | Similarly shaped airfoils
Plain Flapped Shapes: 25% flap chord | 30% flap chord | 35% flap chord | 40% flap chord
Basic Data: cl vs α | cd vs α | cm vs α | cl/cd vs α | cd vs cl | cl/cd vs cl | cl vs cd | cm vs cl | Curve fits | Lift curve slopes
Data source comparison (Codes, CFD, Wind tunnel)
Compressibility Effects: cl vs α | cd vs α | cm vs α | cl/cd vs α | cd vs cl | cl/cd vs cl | cl vs cd | cm vs cl
Roughness Effects: cl vs α | cd vs α | cm vs α | cl/cd vs α | cd vs cl | cl/cd vs cl | cl vs cd | cm vs cl
Plain Flap Effects: cl,max vs flap deflection: all flap chords | 25% flap chord | 30% flap chord | 35% flap chord | 40% flap chord
Plain Flap Effects: cl vs α for various flap deflections: 25% flap chord | 30% flap chord | 35% flap chord | 40% flap chord
Plain Flap Effects: cm vs α for various flap deflections: 25% flap chord | 30% flap chord | 35% flap chord | 40% flap chord
Plain Flap Effects: cd vs α for various flap deflections: 25% flap chord | 30% flap chord | 35% flap chord | 40% flap chord
Disclaimer: All information presented herein is delivered without guarantee or warranty of any kind. The user assumes the entire risk of use of this information.
2. DP1.72/8.32_DS
3. DP1.72/8.16_DS
4. DP1.82/8.21_DS
5. DP1.87/9.07_DS
6. DP1.79/8.37_DS
7. BOEING 707 .54 SPAN
8. DP2.06/8.67_DS
9. KC-135 BL351.6
10. BOEING 707 .99 SPAN
11. TP50-DS
12. NACA65-309 a=0.0
13. DP2.05/8.65_DS
14. S2055
15. NACA65-309 a=0.2
16. MH 23 8%
17. RG 14
18. NACA65-309
19. NACA65-209 a=0.6
20. NACA65-209 a=0.5
21. NACA65A309